Aerocapture Assessment for NASA Ice Giants Pre-Decadal Survey Mission Study
Aerodynamic Analysis of an Entry Capsule at Titan in Transition Regime
Aerodynamic Design of Nozzles with Uniform Outflow for Hypervelocity Ground-Test Facilities
A method is proposed for the aerodynamic design of nozzles with uniform outflow for supersonic and hypersonic ground-test facilities
...Aero Engine Ceramics—the Vision, the Reality and the Progress
Aerothermodynamic Analysis of High-Altitude Space Launcher with Direct-Simulation Monte Carlo Method
Aerothermodynamic Assessment of Spiked Configuration for Drag Reduction at Hypersonic Speeds
Aerothermodynamics Behind a Blunt Body at Superorbital Speeds
A field test study of leaf contamination on railhead surfaces
A finite-volume-based two-dimensional wall-flow diesel particulate filter regeneration model
Afterburning Effects on Thermal Environment of Liquid Oxygen/Kerosene Rocket Under Low Altitudes